STC SA8204SW-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA82045W.D This certificate issued to: RAM Aircraft, Limited Partnership 7505 Karl May Drive Waco, IX 76708 Certifies that the change in the type design for the following product with the limitations and conditions therofor as spocified hereon meets the airworthiness requirement's of Part 3 of the Civil Air Regulations.

Original Product Typo Certificate Number: A7CE Make: Cessna Model: 414A Description of Type Design Change: Option 1. Installation of Vortex Generators on a Cessna model 414A modified in accordance with STC number SA7633SW-D and in accordance with RAM Aircraft, Limited Partnership RAM drawing 1536, dated December 31, 1991 or later FAA approved revision. No change to the Airplane Flight Manual Supplement (AFMS), dated August 10, 1989. Option 2 Installation of Vortex Generators in accordance with RAM Aircraft, Limited Partnership RAM drawing 1536, dated December 31,1991 or later FAA approved revision. See option 2 in limitations for appropriate AFMS.

Date of Application: January 10, 1992 Date Reissued: October 8, 2001; February 28, 2008; August 29, 2008 Date of Issuance: February 10, 1992 Date Amended:

FEDERAL AVIATION ORIGINAL SIGNED BY TERRY BOWDEN (Signature) Terry L. Bowden DAS administrator DAS-700100-SW TOMINISTRATO RAM Aircraft LP Waco, Texas (Title) ration of this certaticate js punishable by a lane of not exceeding 91,000, or imprisonment not exceeding 3 years, or both.

ificate may be transferred in accordance with FAR 21.47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA82045W-D Date of Issuance: February 10, 1992 Reissuance Date: August 29, 2008 Limitations and Conditions: (Continued): Option 2. Aircraft Flight Manual Supplement - FM1026 dated February 10, 1992 is required. Airspeed markings and limitations placards to show new approved stall speeds and minimum control speeds must be installed to agree with the Aircraft Flight Manual Supplement. Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence

FAA Form 8110-1-1(10-69) - Fage 3 of 3